Accession Number:

ADD005260

Title:

Shock-Excursion Apparatus for Retracting the Umbilical Plug of a Missile.

Descriptive Note:

Patent,

Corporate Author:

DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s):

Report Date:

1978-06-06

Pagination or Media Count:

6.0

Abstract:

A flexible wire is secured at one end to the umbilical plug and at the other to a sheave of a rotary actuator. The actuator is driven by launch-gas pressure to reel in the wire and retract the plug. A plug stop is mounted on the launch tube in the path of travel of the plug. Lift-off of the missile carries the plug into the stop to disengage and free it for retraction. The flexible wire coupling is provided with a slack portion to accommodate shock excursions and assure disengagement of the plug prior to retraction. Author

Subject Categories:

  • Guided Missile Launching and Basing Support
  • Ground Support Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE